Man-machine function allocation method of civil aircraft cockpit
A civil aircraft cockpit and function allocation technology, applied in special data processing applications, instruments, electrical digital data processing, etc., can solve problems such as no systematic and complete method, and no public reports on core technologies
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[0080] The following takes a function "Fault Diagnosis (FD)" in the cockpit of a civil aircraft as an example to illustrate the specific implementation process of the above function allocation, that is, to use the proposed method to determine the optimal automation level of FD.
[0081] 1. Determine the set of human and machine superior capabilities H={h 1 , h 2 , h 3 , h 4 , h 5 , h 6 , h 7 , h 8} and M={m 1 , m 2 , m 3 , m 4 , m 5 , m 6 , m 7 , m 8}, the meaning of each element is shown in Table 1.
[0082] 2. Using the AHP to obtain the weight vectors of the elements in H and M, respectively:
[0083] ω=(0.287, 0.106, 0.081, 0.142, 0.119, 0.019, 0.193, 0.053)
[0084] ξ=(0.163, 0.097, 0.228, 0.126, 0.154, 0.106, 0.062, 0.064)
[0085] 3. Its FD function is divided into 10 automation levels, according to the degree of automation from low to high:
[0086] x 1 : The system does not provide any assistance, the pilot must complete all decisions and maneuvers
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